Sizing of an Aircraft Fuel Pump
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A need to pump a mixture of two-phase fluid appears naturally in many situations. One example of this situation is aircraft fuel systems, where the pump inlet may have two-phase mixture due to the desorption of the dissolved gases at low pressures at higher altitudes. A simple procedure of selecting proper design conditions for the inlet inducer and a method of sizing the inducer, impeller and volute to meet all the design requirements has been described. This procedure has also been applied to a typical fighter plane boost pump design.
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2011 ◽
Vol 69
(4)
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pp. 842-858
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2006 ◽
Vol 72
(719)
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pp. 1781-1788
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